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Volumn 27, Issue 6, 2004, Pages 1096-1102

Lyapunov-based nonlinear missile guidance

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; KINEMATICS; MANEUVERABILITY; MISSILES; NONLINEAR SYSTEMS; STATE SPACE METHODS; SYSTEM STABILITY;

EID: 10044287394     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.8629     Document Type: Article
Times cited : (77)

References (16)
  • 1
    • 33845737702 scopus 로고    scopus 로고
    • Progress in Astronautics and Aeronautics, AIAA, Reston, VA
    • Zarchan, P., Tactical and Strategic Missile Guidance, Vol. 199, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2002, pp. 11-29.
    • (2002) Tactical and Strategic Missile Guidance , vol.199 , pp. 11-29
    • Zarchan, P.1
  • 2
    • 0015094840 scopus 로고
    • Optimal intercept guidance for short-range tactical missiles
    • Cottrel, R. G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol. 9, No. 7, 1971, pp. 1414, 1415.
    • (1971) AIAA Journal , vol.9 , Issue.7 , pp. 1414
    • Cottrel, R.G.1
  • 3
    • 0026154544 scopus 로고
    • Optimal guidance for high-order and acceleration constrained missile
    • Rusnak, I., and Meir, L., "Optimal Guidance for High-Order and Acceleration Constrained Missile," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 3, 1991, pp. 589-596.
    • (1991) Journal of Guidance, Control, and Dynamics , vol.14 , Issue.3 , pp. 589-596
    • Rusnak, I.1    Meir, L.2
  • 4
    • 0018492188 scopus 로고
    • On optimal guidance for homing missiles
    • Gutman, S., "On Optimal Guidance for Homing Missiles," Journal of Guidance, Control, and Dynamics, Vol. 2, No. 4, 1979, pp. 296-300.
    • (1979) Journal of Guidance, Control, and Dynamics , vol.2 , Issue.4 , pp. 296-300
    • Gutman, S.1
  • 5
    • 0032028247 scopus 로고    scopus 로고
    • Geometric approach to three-dimensional missile guidance problem
    • Chiou, Y. C., and Kuo, C. Y., "Geometric Approach to Three-Dimensional Missile Guidance Problem," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 2, 1998, pp. 335-341.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.2 , pp. 335-341
    • Chiou, Y.C.1    Kuo, C.Y.2
  • 6
    • 0035393352 scopus 로고    scopus 로고
    • Design of missile guidance law via variable structure control
    • Moon, J., Kim, K., and Kim, Y, "Design of Missile Guidance Law via Variable Structure Control," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 4, 2001, pp. 659-664.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.4 , pp. 659-664
    • Moon, J.1    Kim, K.2    Kim, Y.3
  • 7
    • 0042303798 scopus 로고    scopus 로고
    • Zero-miss distance guidance law based on line-of-sight rate measurement only
    • Gurfil, P., "Zero-Miss Distance Guidance Law Based on Line-of-Sight Rate Measurement Only," Control Engineering Practice, Vol. 11, No. 7, 2003, pp. 819-832.
    • (2003) Control Engineering Practice , vol.11 , Issue.7 , pp. 819-832
    • Gurfil, P.1
  • 9
    • 0036057175 scopus 로고    scopus 로고
    • Guidance against maneuvering targets using lyapunov optimizing feedback control
    • IEEE Press, New York
    • Vincent, T. L., and Morgan, R., "Guidance Against Maneuvering Targets Using Lyapunov Optimizing Feedback Control," Proceedings of the American Control Conference, IEEE Press, New York, 2002, pp. 215-220.
    • (2002) Proceedings of the American Control Conference , pp. 215-220
    • Vincent, T.L.1    Morgan, R.2
  • 10
    • 85087191702 scopus 로고    scopus 로고
    • A new approach to guidance law design
    • Aug.
    • Yanushevsky, R. T., and Boord, W. J., "A New Approach to Guidance Law Design," AIAA Paper 2003-5577, Aug. 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.5577
    • Yanushevsky, R.T.1    Boord, W.J.2
  • 11
    • 0014814621 scopus 로고
    • Estimating optimal tracking filter performance manned maneuvering targets
    • Singer, R. A., "Estimating Optimal Tracking Filter Performance Manned Maneuvering Targets," IEEE Transactions on Aerospace and Electronic Systems, Vol. 6, No. 4, 1970, pp. 473-483.
    • (1970) IEEE Transactions on Aerospace and Electronic Systems , vol.6 , Issue.4 , pp. 473-483
    • Singer, R.A.1
  • 12
    • 0142154929 scopus 로고    scopus 로고
    • On the need for integrated estimation/guidance design for hit-to-kill accuracy
    • American Automatic Control Council. Evanston, IL
    • Shinar, J., Oshman, Y., and Turetsky, V., "On the Need for Integrated Estimation/Guidance Design for Hit-to-Kill Accuracy," Proceedings of the American Control Conference. American Automatic Control Council. Evanston, IL. 2003. pp. 402-407.
    • (2003) Proceedings of the American Control Conference , pp. 402-407
    • Shinar, J.1    Oshman, Y.2    Turetsky, V.3
  • 13
    • 85086614390 scopus 로고    scopus 로고
    • Circular navigation missile guidance with incomplete information and uncertain autopilot model
    • Aug.
    • Manchester, I. R., and Savkin, A. V., "Circular Navigation Missile Guidance with Incomplete Information and Uncertain Autopilot Model." AIAA Paper 2003-5448, Aug. 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.5448
    • Manchester, I.R.1    Savkin, A.V.2
  • 14
    • 0033746930 scopus 로고    scopus 로고
    • Optimal guidance laws with uncertain time-of-flight
    • Rusnak, I., "Optimal Guidance Laws with Uncertain Time-of-Flight." IEEE Transactions on Aerospace and Electronics Systems. Vol. 36, No. 2. 2000, pp. 721-725.
    • (2000) IEEE Transactions on Aerospace and Electronics Systems , vol.36 , Issue.2 , pp. 721-725
    • Rusnak, I.1
  • 15
    • 0004178386 scopus 로고    scopus 로고
    • Prentice - Hall, Upper Saddle River, NJ
    • Khalil, H. K., Nonlinear Systems, second ed., Prentice - Hall, Upper Saddle River, NJ. 1996, pp. 211-216.
    • (1996) Nonlinear Systems, Second Ed. , pp. 211-216
    • Khalil, H.K.1
  • 16


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.